CN206177549U - Variable flow field burning test device of constant volume - Google Patents

Variable flow field burning test device of constant volume Download PDF

Info

Publication number
CN206177549U
CN206177549U CN201621114879.3U CN201621114879U CN206177549U CN 206177549 U CN206177549 U CN 206177549U CN 201621114879 U CN201621114879 U CN 201621114879U CN 206177549 U CN206177549 U CN 206177549U
Authority
CN
China
Prior art keywords
main body
constant volume
valve
jet nozzle
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201621114879.3U
Other languages
Chinese (zh)
Inventor
何小明
龙伟成
翟逸轩
胡新源
苗明达
侯凯
陈毅华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing University of Aeronautics and Astronautics
Original Assignee
Nanjing University of Aeronautics and Astronautics
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CN201621114879.3U priority Critical patent/CN206177549U/en
Application granted granted Critical
Publication of CN206177549U publication Critical patent/CN206177549U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

The utility model discloses a variable flow field burning test device of constant volume, variable flow field burning test device of constant volume wherein, including main body, gas distribution system, oil feeding system, ignition system, observing and controlling system and fluidic system, gas distribution system, fluidic system, oil feeding system, ignition system all link to each other with the observing and controlling system, main body links to each other with the observing and controlling system, gas distribution system, fluidic system, oil feeding system, ignition system all link to each other with main body. The utility model discloses can change direction and the position of jet nozzle, fluidic pressure. And the air current that production institute that can reduce cost needs.

Description

Constant volume variable air flow fields corrosion chamber
Technical field:
The utility model is related to a kind of constant volume variable air flow fields corrosion chamber, and it is applied to the different flow fields of research to burning Impact.
Background technology:
The development of engine is all the time based on propulsion power, the lifting of economy and the decline of exhaust emission Research direction is wanted, the development key problem of engine is the improvement of burning.One of direction of research burning is change burning Indoor Study on Flow Field improves the air current flow mode of efficiency of combustion.
Engine combustion Indoor Flow Field is complicated, and flow field formative factor is complicated, and flow field control is difficult.Traditional flow field generation side Formula is to change piston and top of combustion chamber shape to remove the different air-flow of generations, the required flow field time cost of generation and price into This height.
It is, thus, sought for the mode that a kind of low cost changes flow field goes to test impact of more flow fields to burning, enter And improve Efficiency of the different flow fields of research to combustion effects.
Utility model content:
In order to improve Efficiency of the research flow field to combustion effects, the utility model provides a kind of constant volume variable air flow fields combustion Experimental rig is burnt, different flow fields can efficiently generated on the basis of realization burning, can be produced at short notice different Flow field.
The utility model is adopted the following technical scheme that:A kind of constant volume variable air flow fields corrosion chamber, including main body, match somebody with somebody Gas system, oil supply system, ignition system, TT&C system and fluidic system, the air distribution system, fluidic system, oil supply system, Ignition system is connected with TT&C system, and the main body is connected with TT&C system, the air distribution system, fluidic system, fuel feeding System, ignition system are connected with main body.
Further, the air distribution system includes the spray of air pump, magnetic valve, intake valve, check valve, air bleeding valve and jet Mouth, the delivery outlet point two-way of air pump is respectively connected to intake valve and magnetic valve, and intake valve connects main body, and magnetic valve connection is unidirectional Valve, check valve connection jet nozzle, jet nozzle connects main body, and main body connects air bleeding valve.
Further, the main body is provided with combustion chamber, and jet nozzle is arranged on main bullet body sidewall, the spray of jet nozzle Mouth is indoor in burning.
The utility model is also adopted the following technical scheme that:A kind of method of work of constant volume variable air flow fields corrosion chamber, Comprise the steps:
(1). TT&C system collection installed in it is main bullet body sidewall sensor signal, sensor include temperature sensor with Pressure sensor, sensor connects main body combustion chamber, obtains the working condition of the combustion chamber of main body, judges main body Working condition;
(2). air distribution system controls air pump and provides bleed pressure by TT&C system, and by TT&C system inlet open is controlled Close realize main body combustion chamber is carried out initial press with it is burned after scavenging;
(3). TT&C system control air pump produces air pressure potential source, and TT&C system controls burning of the INO to main body Room carries out being pressurized to initial pressure value, closes intake valve, and fluidic system controls magnetic valve and uses higher than initial by TT&C system The pressure value of pressure forms pressure differential and produces flow field with internal pressure of combustion chamber, and by oil supply system oil spout main body combustion chamber is entered Interior, ignition system lights the indoor igniting of main body burning, and so as to burn in the case where flow field is generated, TT&C system control air bleeding valve is opened Tail gas after burning is discharged, TT&C system control INO carries out scavenging to combustion chamber.
The utility model has the advantages that:
(1) direction and position, the pressure of jet of jet nozzle can, be changed.
(2) air-flow required for generation research that, can be inexpensive.
Description of the drawings:
Fig. 1 is the structure chart of constant volume variable air flow fields corrosion chamber.
Fig. 2 is fluidic system structure chart.
Fig. 3 is jet nozzle scheme of installation.
Specific embodiment:
Refer to shown in Fig. 1, the utility model constant volume variable air flow fields corrosion chamber includes main body 104, distribution system System 101, oil supply system 105, ignition system 106, TT&C system 103 and fluidic system 102, air distribution system 101, fluidic system 102nd, oil supply system 105, ignition system 106 are connected with TT&C system 103, and main body 104 is connected with TT&C system 103, matches somebody with somebody Gas system 101, fluidic system 102, oil supply system 105, ignition system 106 are connected with main body 104.
Refer to shown in Fig. 2, air distribution system 101 includes air pump 201, magnetic valve 202, intake valve 203, check valve 204, row Air valve 205 and jet nozzle 206, the delivery outlet point two-way of air pump 201 is respectively connected to intake valve 203 and magnetic valve 202, air inlet Valve 203 connects main body 104, the connection check valve 204 of magnetic valve 202, the connection jet nozzle 206 of check valve 204, jet nozzle The main body 104 of 206 connections, the connection air bleeding valve 205 of main body 104.
Refer to shown in Fig. 3, the combuster of main body 104, jet nozzle 206 is arranged on the side wall of main body 104, spout It is indoor in burning.
The method of work of the utility model constant volume variable air flow fields corrosion chamber, comprises the steps:
(1). the collection of TT&C system 103 is arranged on the signal of the sensor of the side wall of main body 104, and sensor includes that temperature is passed Sensor and pressure sensor, sensor connects the main combustion chamber of body 104, obtains the work shape of the combustion chamber of main body 104 State, judges the working condition of main body 104;
(2). air distribution system 101 controls air pump 201 and provides bleed pressure by TT&C system 103, by TT&C system 103 Control intake valve 203 switch realize the combustion chamber of main body 104 is carried out initial press with it is burned after scavenging;
(3). the control air pump 201 of TT&C system 103 produces air pressure potential source, and the control intake valve 203 of TT&C system 103 opens right The combustion chamber of main body 104 carries out being pressurized to initial pressure value, closes intake valve 203, and fluidic system 102 passes through TT&C system 103 control magnetic valves 202 form pressure differential and produce flow field using the pressure value higher than initial pressure and internal pressure of combustion chamber, pass through The oil spout of oil supply system 105 is burnt interior into main body 104, and ignition system 106 is lighted main body 104 and burnt indoor igniting, from And burn in the case where flow field is generated, the control air bleeding valve 205 of TT&C system 103 is opened and discharges tail gas after burning, and TT&C system 103 is controlled Intake valve 203 is opened, and to combustion chamber scavenging is carried out.
Fig. 3 is the scheme of installation of jet nozzle, changes different jet nozzles, by the length for changing jet nozzle 206 The position and injection method of degree, width, Angulation changes nozzle in combustion chamber, reaches the purpose for changing flow field direction.Before the test, According to the flow field that test needs, the jet nozzle 206 of suitable fluidic system 102 is installed.The device quickly can be produced effectively not Same flow field is used for combustion test.
The above is only preferred embodiment of the present utility model, it is noted that for the common skill of the art For art personnel, some improvement can also be made on the premise of without departing from the utility model principle, these improvement also should be regarded as Protection domain of the present utility model.

Claims (3)

1. a kind of constant volume variable air flow fields corrosion chamber, it is characterised in that:Including main body (104), air distribution system (101), Oil supply system (105), ignition system (106), TT&C system (103) and fluidic system (102), the air distribution system (101), Fluidic system (102), oil supply system (105), ignition system (106) are connected with TT&C system (103), the main body (104) it is connected with TT&C system (103), the air distribution system (101), fluidic system (102), oil supply system (105), igniting system System (106) is connected with main body (104).
2. constant volume variable air flow fields corrosion chamber as claimed in claim 1, it is characterised in that:The air distribution system (101) Including air pump (201), magnetic valve (202), intake valve (203), check valve (204), air bleeding valve (205) and jet nozzle (206), the delivery outlet of air pump (201) point two-way is respectively connected to intake valve (203) and magnetic valve (202), intake valve (203) connection Main body (104), magnetic valve (202) connection check valve (204), check valve (204) connection jet nozzle (206), jet nozzle (206) main body (104), main body (104) connection air bleeding valve (205) are connected.
3. constant volume variable air flow fields corrosion chamber as claimed in claim 2, it is characterised in that:The main body (104) sets Combuster, jet nozzle (206) is on the wall of main body (104) side, and the spout of jet nozzle (206) is indoor in burning.
CN201621114879.3U 2016-10-11 2016-10-11 Variable flow field burning test device of constant volume Active CN206177549U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621114879.3U CN206177549U (en) 2016-10-11 2016-10-11 Variable flow field burning test device of constant volume

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621114879.3U CN206177549U (en) 2016-10-11 2016-10-11 Variable flow field burning test device of constant volume

Publications (1)

Publication Number Publication Date
CN206177549U true CN206177549U (en) 2017-05-17

Family

ID=58677441

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201621114879.3U Active CN206177549U (en) 2016-10-11 2016-10-11 Variable flow field burning test device of constant volume

Country Status (1)

Country Link
CN (1) CN206177549U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106404337A (en) * 2016-10-11 2017-02-15 南京航空航天大学 Combustion test device of flow field with variable constant volume and work method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106404337A (en) * 2016-10-11 2017-02-15 南京航空航天大学 Combustion test device of flow field with variable constant volume and work method thereof
CN106404337B (en) * 2016-10-11 2019-04-23 南京航空航天大学 Constant volume variable air flow fields corrosion chamber and its working method

Similar Documents

Publication Publication Date Title
CN103477061B (en) Gas engine, the control device of gas engine and control method
CN103154474B (en) The method of the stoichiometric explosive motor of vaporized fuel and operation explosive motor
CN103748334A (en) Two-stroke internal combustion engine, method of operating two-stroke internal combustion engine and method of converting two-stroke engine
CN102374059A (en) Method and device for controlling diesel engine
CN108644034B (en) High-power lean burn natural gas engine combustion system and method based on ozone to support combustion
CN101403350A (en) Internal combustion directly-heating steam engine
SE7507456L (en) DEVICE AT THE EXHAUST TURBINE.
CN102322332B (en) Combustion chamber structure of CNG (Compressed Natural Gas) engine and fuel injection method thereof
CN110318860A (en) A kind of marine large-diameter natural gas engine combustion system of multistage fuel gas injection
CN110318858A (en) A kind of diesel oil ignited formula natural gas engine combustion system and combustion method
CN202645661U (en) Valve gas compressor
CN206177549U (en) Variable flow field burning test device of constant volume
CN87105408A (en) Pulse-sonic jet combustors (or nozzle)
CN214173744U (en) Constant volume combustion testing device with controllable oxygen concentration
CN106404337B (en) Constant volume variable air flow fields corrosion chamber and its working method
CN214007317U (en) Engine
CN2509335Y (en) Internal combustion engine steam booster
CN205078335U (en) Spark plug triggers formula homogeneity compression ignition engine
CN203130317U (en) Engine provided with common oil and gas nozzle
CN206206020U (en) One kind hydrogenation low pressure EGR system
CN203394631U (en) Engine combustor pressurizing mechanism
CN204851477U (en) Engine fuel feed system
RU78527U1 (en) PISTON ENGINE
CN2813904Y (en) Double-fuel nozzle of engine utilizing waste gas residual-heat
CN205936844U (en) Miller cycle diesel oil natural gas dual -fuel engine

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant